Inventor
THORNTON LANE
US16 patents
⚠️ This page may combine multiple inventors who share the name “THORNTON LANE”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
15 patentsUS9845694B2Dec 19, 2017
Flow directing cover for engine component
UNITED TECHNOLOGIES CORP5 citations83
US10208602B2Feb 19, 2019
Asymmetric diffuser opening for film cooling holes
UNITED TECHNOLOGIES CORP11 citations82
US10458264B2Oct 29, 2019
Seal arrangement for turbine engine component
UNITED TECHNOLOGIES CORP4 citations73
US10655473B2May 19, 2020
Gas turbine engine turbine blade leading edge tip trench cooling
UNITED TECHNOLOGIES CORP2 citations72
US10273809B2Apr 30, 2019
Centrifugal airfoil cooling modulation
UNITED TECHNOLOGIES CORP4 citations72
US11781439B2Oct 10, 2023
Seal arrangement for turbine engine component
UNITED TECHNOLOGIES CORP0 citations62
US10844730B2Nov 24, 2020
Centrifugal airfoil cooling modulation
UNITED TECHNOLOGIES CORP1 citations62
US10738619B2Aug 11, 2020
Fan cooling hole array
UNITED TECHNOLOGIES CORP1 citations62
US10259039B2Apr 16, 2019
Gas turbine engine component cooling passage and space casting core
UNITED TECHNOLOGIES CORP1 citations62
US10196915B2Feb 5, 2019
Trailing edge platform seals
UNITED TECHNOLOGIES CORP1 citations61
US10821500B2Nov 3, 2020
Lost core molding cores for forming cooling passages
UNITED TECHNOLOGIES CORP0 citations52
US10005123B2Jun 26, 2018
Lost core molding cores for forming cooling passages
UNITED TECHNOLOGIES CORP0 citations52
US10465543B2Nov 5, 2019
Flow directing cover for engine component
UNITED TECHNOLOGIES CORP0 citations51
US10400607B2Sep 3, 2019
Large-footprint turbine cooling hole
UNITED TECHNOLOGIES CORP0 citations51
US10370979B2Aug 6, 2019
Baffle for a component of a gas turbine engine
UNITED TECHNOLOGIES CORP0 citations51